Turbojet engine exhaust casing with integral suspension lugs
US5259183A · kind A · utility
20Cited by
4References
3Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jun 17, 1992 |
| Grant date | Nov 9, 1993 |
| Priority date | — |
| Expiry date | Jun 17, 2012 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2230/642
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The exhaust casing of a turbojet engine has a polygonal cross-section and carries at least three hanging lugs provided with holes designed to receive fixing axles of a rear suspension structure for the engine. The axes of these holes are situated at vertices of the polygon defined by the cross-section of the casing, and this polygon is regular except at the position of each of the hanging lugs, where it is deformed to displace the respective vertex radially outward.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.